Statements (61)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:aircraft
|
gptkbp:bfsLayer |
4
|
gptkbp:bfsParent |
gptkb:Kazakh_Air_Force
gptkb:Georgian_Air_Force gptkb:Cuban_Air_Force gptkb:Transnistrian_Air_Force |
gptkbp:crew |
2
|
gptkbp:design |
aerobatic training
|
gptkbp:engine |
gptkb:Vedeneyev_M14_P
|
gptkbp:first_flight |
gptkb:1976
|
gptkbp:height |
2.60 m
|
https://www.w3.org/2000/01/rdf-schema#label |
Yak-52
|
gptkbp:is_used_by |
various air forces
|
gptkbp:length |
8.20 m
|
gptkbp:manufacturer |
gptkb:Yakovlev
|
gptkbp:max_speed |
300 km/h
|
gptkbp:max_takeoff_weight |
1,200 kg
|
gptkbp:notable_feature |
all-metal construction
low operating costs tailwheel landing gear used in airshows good fuel efficiency dual control system low-wing monoplane design simple maintenance easy to fly stable flight characteristics good visibility from cockpit popular among flying schools robust landing gear large cockpit space can be equipped with smoke system can be fitted with floats for water landings can be used for aerobatic competitions can be used for basic flight training can be used for formation flying can be used for glider towing can be used for instrument training can be used for night flying training can perform spins and loops good aerobatic performance has a good climb rate has a good glide ratio has a good roll rate has a large baggage compartment has a large fuel tank capacity has a retractable landing gear option has a strong airframe |
gptkbp:number_built |
over 1,000
|
gptkbp:origin |
gptkb:Monarch
|
gptkbp:power_output |
360 hp
|
gptkbp:production_years |
gptkb:1976
gptkb:1998 |
gptkbp:range |
1,000 km
|
gptkbp:role |
gptkb:aircraft
|
gptkbp:service_ceiling |
4,500 m
|
gptkbp:speed |
90 km/h
|
gptkbp:variant |
gptkb:Yak-52_M
gptkb:Yak-52_U gptkb:Yak-52_W |
gptkbp:wingspan |
9.80 m
|